CN214036391U - Aluminum alloy plate for ship - Google Patents

Aluminum alloy plate for ship Download PDF

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Publication number
CN214036391U
CN214036391U CN202023305729.XU CN202023305729U CN214036391U CN 214036391 U CN214036391 U CN 214036391U CN 202023305729 U CN202023305729 U CN 202023305729U CN 214036391 U CN214036391 U CN 214036391U
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CN
China
Prior art keywords
plate
aluminum alloy
alloy plate
wing
groove
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Expired - Fee Related
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CN202023305729.XU
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Chinese (zh)
Inventor
刘辰煜
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Haian Huada Aluminum Profile Co Ltd
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Haian Huada Aluminum Profile Co Ltd
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Priority to CN202023305729.XU priority Critical patent/CN214036391U/en
Application granted granted Critical
Publication of CN214036391U publication Critical patent/CN214036391U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model relates to an aluminum alloy section bar technical field especially relates to a marine aluminum alloy plate, now proposes following scheme, and it includes: the upper aluminum alloy plate is arranged at the upper part of the lower aluminum alloy plate; the first wing plates on the left side and the right side of the upper aluminum alloy plate are covered on the outer sides of the second wing plates on the left side and the right side of the lower aluminum alloy plate; the side of the bottom wing plate at the lower part of the upper aluminum alloy plate extends towards the bottom of the first wing plate, and the outer side edge of the bottom wing plate and the outer side surface of the first wing plate above the bottom wing plate are arranged in the same vertical line; a plurality of fixing pieces are arranged between the upper aluminum alloy plate and the lower aluminum alloy plate; heat insulation board assemblies are arranged among the adjacent fixing pieces, between the fixing piece positioned at the leftmost side and the second wing plate positioned at the left side and between the fixing piece positioned at the rightmost side and the second wing plate positioned at the right side; the pressure resistance of the aluminum alloy plate is improved, and the service life of the aluminum alloy plate is prolonged.

Description

Aluminum alloy plate for ship
Technical Field
The utility model relates to an aluminum alloy ex-trusions technical field, concretely relates to marine aluminum alloy plate.
Background
The aluminum alloy plate is an industrial building material, is used in various industries according to different materials, and can be divided into two categories of non-painting products and painting products according to the surface treatment mode. The used industries are airplane structures, rivets, missile components, truck hubs, packaging and heat-insulating aluminum foils, heat exchangers, bulkheads, ribs, spars, and the like
At present, be used for marine aluminum alloy in the market, form by the aluminum alloy plate concatenation of a block individual layer structure, long-time the use, the individual layer is yielding to influence the user state of aluminum alloy, the life of aluminum alloy shortens, thereby leads to cost of maintenance and replacement cost to increase, the urgent need to improve.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to prior art's defect and not enough, provide a simple structure, reasonable in design, convenient to use's marine aluminum alloy plate improves aluminum alloy plate's compressive capacity, prolongs aluminum alloy plate's life.
In order to achieve the above object, the utility model adopts the following technical scheme: comprises an upper aluminum alloy plate, a lower aluminum alloy plate and a fixing piece; the upper aluminum alloy plate is arranged at the upper part of the lower aluminum alloy plate; the first wing plates on the left side and the right side of the upper aluminum alloy plate are covered on the outer sides of the second wing plates on the left side and the right side of the lower aluminum alloy plate; the side of the bottom wing plate at the lower part of the upper aluminum alloy plate extends towards the bottom of the first wing plate, and the outer side edge of the bottom wing plate and the outer side surface of the first wing plate above the bottom wing plate are arranged in the same vertical line; a plurality of fixing pieces are arranged between the upper aluminum alloy plate and the lower aluminum alloy plate; and an insulation board assembly is arranged between the adjacent fixing pieces, between the leftmost fixing piece and the left second wing plate and between the rightmost fixing piece and the right second wing plate.
Furthermore, the heat insulation plate component consists of a reinforcing plate, a plastic plate and a heat insulation plate; the left side surface and the right side surface of the heat insulation plate are respectively provided with a plastic plate; the plastic plate is fixedly connected with the reinforcing plate on the groove surface formed by the plastic plate; the left side surface and the right side surface of the fixing piece are provided with third convex blocks; the inner side surfaces of the second wing plates on the left side and the right side are provided with fourth convex blocks; the fourth convex blocks on the left side and the right side are respectively clamped in grooves formed by the reinforcing plates in the heat insulation plate assembly on the leftmost side and the heat insulation plate assembly on the rightmost side; the third bump is clamped in a groove formed by the reinforcing plate adjacent to the third bump.
Furthermore, a first bump is arranged in the middle of the inner side surface of the first wing plate; the first lug is clamped in the first groove in the middle of the second wing plate adjacent to the first lug.
Further, a second groove is formed in the lower side face of the upper wing plate of the upper aluminum alloy plate; a third groove is formed in the lower side face of the bottom wing plate of the lower aluminum alloy plate; the upper side surface and the lower side surface of the fixing piece are provided with second convex bodies; the second convex bodies on the upper side and the lower side are respectively clamped in the second groove and the third groove.
Further, the width of the heat preservation plate assembly is 100mm-250 mm.
Furthermore, the upper surface of the upper wing plate is provided with an anti-skid layer.
After the structure is adopted, the utility model discloses beneficial effect does: a marine aluminum alloy plate, improve aluminum alloy plate's compressive capacity, extension aluminum alloy plate's life, the practicality is stronger, the utility model has the advantages of simple structure sets up rationally, the cost of manufacture is low.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings needed to be used in the description of the embodiments or the prior art will be briefly described below, it is obvious that the drawings in the following description are only some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to these drawings without inventive exercise.
Fig. 1 is a structural view of the present invention.
Fig. 2 is a structural view of the middle and upper aluminum alloy plate of the present invention.
FIG. 3 is a structural view of the middle and lower aluminum alloy plate of the present invention.
Fig. 4 is an enlarged view of a portion a in fig. 1.
Description of reference numerals:
the aluminum-alloy plate comprises an upper aluminum-alloy plate 1, a lower aluminum-alloy plate 2, a fixing part 3, a second convex body 3-1, a third convex block 3-2, a first wing plate 4, a first convex block 4-1, a second wing plate 5, a fourth convex block 5-1, a first groove 5-2, a bottom wing plate 6, a third groove 6-1, an upper wing plate 7, a second groove 7-1, an anti-skid layer 7-2, a reinforcing plate 8, a plastic plate 9, a heat-insulation plate 10 and a heat-insulation plate assembly 11.
Detailed Description
The present invention will be further described with reference to the accompanying drawings.
Referring to fig. 1 to 4, the technical solution adopted by the present embodiment is: comprises an upper aluminum alloy plate 1, a lower aluminum alloy plate 2 and a fixing piece 3; the upper aluminum alloy plate 1 is arranged at the upper part of the lower aluminum alloy plate 2; the first wing plates 4 on the left side and the right side of the upper aluminum alloy plate 1 are covered on the outer sides of the second wing plates 5 on the left side and the right side of the lower aluminum alloy plate 2; the width of the upper aluminum alloy plate 1 is 400 mm; the width of the first wing plate 4 is 20 mm; the width of the second wing plate 5 is 20 mm; the side of the bottom wing plate 6 at the lower part of the upper aluminum alloy plate 1 extends towards the bottom of the first wing plate 4, and the outer side edge of the bottom wing plate 6 and the outer side surface of the first wing plate 4 above the bottom wing plate are arranged in the same vertical line; the fixing piece 3 is arranged between the upper aluminum alloy plate 1 and the lower aluminum alloy plate 2; insulation board assemblies 11 are arranged between the leftmost fixing member 3 and the left second wing 5 and between the rightmost fixing member 3 and the right second wing 5.
Further, the heat insulation plate assembly 11 consists of a reinforcing plate 8, a plastic plate 9 and a heat insulation plate 10; the left side surface and the right side surface of the heat insulation plate 10 are fixedly provided with plastic plates 9 through gluing; the plastic plate 9 is fixedly connected with the reinforcing plate 8 on the groove surface formed by the plastic plate; the left side surface and the right side surface of the fixing piece 3 are provided with third convex blocks 3-2; the inner side surfaces of the second wing plates 5 on the left side and the right side are provided with fourth convex blocks 5-1; the fourth bumps 5-1 on the left side and the right side are respectively clamped in grooves formed by the reinforcing plates 8 in the heat insulation plate assembly 11 on the leftmost side and the heat insulation plate assembly 11 on the rightmost side; the third bump 3-2 is clamped in a groove formed by the reinforcing plate 8 adjacent to the third bump.
Furthermore, a first bump 4-1 is arranged in the middle of the inner side surface of the first wing plate 4; the first lug 4-1 is clamped in the first groove 5-2 in the middle of the second wing plate 5 adjacent to the first lug; the first lug 4-1 is matched with the first groove 5-2, so that the upper aluminum alloy plate 1 and the lower aluminum alloy plate 2 can be installed.
Further, a second groove 7-1 is formed in the lower side face of the upper wing plate 7 of the upper aluminum alloy plate 1; a third groove 6-1 is formed in the lower side face of the bottom wing plate 6 of the lower aluminum alloy plate 2; the upper side surface and the lower side surface of the fixing piece 3 are provided with second convex bodies 3-1; the width of the fixing piece 3 is 30 mm; the second convex bodies 3-1 on the upper side and the lower side are respectively clamped in the second groove 7-1 and the third groove 6-1; the fixing piece 3 is installed through the matching of the second convex body 3-1, the second groove 7-1 and the third groove 6-1.
Further, the width of the heat preservation plate assembly 11 is 100mm-250 mm.
Further, an anti-slip layer 7-2 is fixed on the upper surface of the upper wing plate 7 through welding; the anti-skid layer 7-2 plays a role of anti-skid and increases the friction force when the ship is used.
Principle of this embodiment: when the aluminum alloy plate is used, the upper aluminum alloy plate 1 and the lower aluminum alloy plate 2 are prepared, then the assembly is started, the first lug 4-1 is clamped in the first groove 5-2, and the outer side edge of the bottom wing plate 6 and the outer side surface of the first wing plate 4 above the bottom wing plate are arranged in the same vertical line; then preparing a fixing plate, respectively clamping and arranging the fixing plate in a second groove 7-1 and a third groove 6-1 through a second convex body 3-1, and after the fixing plate is installed, respectively clamping and arranging a fourth convex block 5-1 and a third convex block 3-2 in grooves formed by a reinforcing plate 8, and completing installation of the heat preservation plate assembly 11; the reinforcing plate 8 can effectively increase the strength of the corner of the heat insulation plate assembly 11, and the heat insulation plate 10 is prevented from deforming in the installation process; when using, can set up the quantity of fixed plate according to the width of last aluminum alloy plate 1 and lower aluminum alloy plate 2, improve aluminum alloy plate's compressive capacity, avoid warping, guarantee aluminum alloy plate's life.
After adopting above-mentioned structure, this embodiment's beneficial effect does:
1. the aluminum alloy plate is formed by combining an upper aluminum alloy plate 1 and a lower aluminum alloy plate 2, the compression resistance of the aluminum alloy plate is convenient to improve through the combination of the upper aluminum alloy plate 1 and the lower aluminum alloy plate 2, so that the service life of the ship is prolonged when the ship is used, meanwhile, a fixing part 3 is arranged between the upper aluminum alloy plate 1 and the lower aluminum alloy plate 2, the stress uniformity of the aluminum alloy plate can be ensured, and the heat insulation plate assembly 11 is arranged, so that the heat insulation effect can be achieved, the gap between the upper aluminum alloy plate 1 and the lower aluminum alloy plate 2 can be filled, the manufacturing cost is reduced, the deformation caused by the uneven stress in long-time use is avoided, and the service life of the aluminum alloy plate is prolonged;
2. the first bump 4-1 is clamped in the first groove 5-2, so that the possibility of deviation of the upper aluminum alloy plate 1 and the lower aluminum alloy plate 2 during installation is avoided, and the installation precision of the aluminum alloy plates is improved; the second convex body 3-1 is clamped in the second groove 7-1 and the third groove 6-1 respectively, so that the situation that the fixed piece 3 is deviated from the upper aluminum alloy plate 1 and the lower aluminum alloy plate 2 during installation is avoided; the fourth bump 5-1 and the third bump 3-2 are respectively clamped in a groove formed in the reinforcing plate 8; guarantee 11 installation accuracy of heated board subassembly, and long-time the use can not warp yet, increase its life.
The above description is only for the purpose of illustrating the technical solutions of the present invention and not for the purpose of limiting the same, and other modifications or equivalent replacements made by those of ordinary skill in the art to the technical solutions of the present invention should be covered within the scope of the claims of the present invention as long as they do not depart from the spirit and scope of the technical solutions of the present invention.

Claims (6)

1. The utility model provides a marine aluminum alloy plate which characterized in that: comprises an upper aluminum alloy plate (1), a lower aluminum alloy plate (2) and a fixing piece (3); the upper aluminum alloy plate (1) is arranged at the upper part of the lower aluminum alloy plate (2); the first wing plates (4) on the left and right sides of the upper aluminum alloy plate (1) are covered on the outer sides of the second wing plates (5) on the left and right sides of the lower aluminum alloy plate (2); the side of the bottom wing plate (6) at the lower part of the upper aluminum alloy plate (1) extends towards the bottom of the first wing plate (4), and the outer side edge of the bottom wing plate (6) and the outer side surface of the first wing plate (4) above the bottom wing plate are arranged in the same vertical line; a plurality of fixing pieces (3) are arranged between the upper aluminum alloy plate (1) and the lower aluminum alloy plate (2); and heat preservation plate assemblies (11) are arranged between the adjacent fixing pieces (3), between the fixing piece (3) at the leftmost side and the second wing plate (5) at the left side, and between the fixing piece (3) at the rightmost side and the second wing plate (5) at the right side.
2. The marine aluminum alloy panel of claim 1, wherein: the heat insulation plate component (11) consists of a reinforcing plate (8), a plastic plate (9) and a heat insulation plate (10); the left side surface and the right side surface of the heat insulation plate (10) are respectively provided with a plastic plate (9); the plastic plate (9) is fixedly connected with the reinforcing plate (8) on the groove surface formed by the plastic plate; the left side surface and the right side surface of the fixing piece (3) are provided with third convex blocks (3-2); the inner side surfaces of the second wing plates (5) on the left side and the right side are provided with fourth convex blocks (5-1); the fourth convex blocks (5-1) on the left side and the right side are respectively clamped in grooves formed by the heat insulation plate component (11) on the leftmost side and the reinforcing plate (8) in the heat insulation plate component (11) on the rightmost side; the third bump (3-2) is clamped in a groove formed by the reinforcing plate (8) adjacent to the third bump.
3. The marine aluminum alloy panel of claim 1, wherein: a first bump (4-1) is arranged in the middle of the inner side surface of the first wing plate (4); the first bump (4-1) is clamped in the first groove (5-2) in the middle of the second wing plate (5) adjacent to the first bump.
4. The marine aluminum alloy panel of claim 1, wherein: a second groove (7-1) is formed in the lower side face of the upper wing plate (7) of the upper aluminum alloy plate (1); a third groove (6-1) is formed in the lower side face of the bottom wing plate (6); the upper side surface and the lower side surface of the fixing piece (3) are provided with second convex bodies (3-1); the second convex bodies (3-1) at the upper side and the lower side are respectively clamped in the second groove (7-1) and the third groove (6-1).
5. The marine aluminum alloy panel of claim 2, wherein: the width of the heat preservation plate component (11) is 100mm-250 mm.
6. The marine aluminum alloy panel of claim 4, wherein: the upper surface of the upper wing plate (7) is provided with an anti-skid layer (7-2).
CN202023305729.XU 2020-12-30 2020-12-30 Aluminum alloy plate for ship Expired - Fee Related CN214036391U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202023305729.XU CN214036391U (en) 2020-12-30 2020-12-30 Aluminum alloy plate for ship

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202023305729.XU CN214036391U (en) 2020-12-30 2020-12-30 Aluminum alloy plate for ship

Publications (1)

Publication Number Publication Date
CN214036391U true CN214036391U (en) 2021-08-24

Family

ID=77344350

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202023305729.XU Expired - Fee Related CN214036391U (en) 2020-12-30 2020-12-30 Aluminum alloy plate for ship

Country Status (1)

Country Link
CN (1) CN214036391U (en)

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Granted publication date: 20210824